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US Patent 11920481 Module for turbomachine
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Patent
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Date Filed
December 18, 2020
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Date of Patent
March 5, 2024
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Patent Application Number
17785217
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Patent Citations
US Patent 10815802 Variable vane assemblies configured for non-axisymmetric actuation
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US Patent 11193380 Integrated strut-vane
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US Patent 7549839 Variable geometry inlet guide vane
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US Patent 8182204 Deflector for a gas turbine strut and vane assembly
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US Patent 8347633 Gas turbine engine with variable geometry fan exit guide vane system
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US Patent 8757965 Gas turbine compression system and compressor structure
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US Patent 9068460 Integrated inlet vane and strut
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US Patent 9617864 Seal assembly for a guide vane assembly
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US Patent 9835038 Integrated strut and vane arrangements
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US Patent 9909434 Integrated strut-vane nozzle (ISV) with uneven vane axial chords
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•••
Patent Inventor Names
Cédric Carl Nathan Cracco
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11920481
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Patent Primary Examiner
Justin D Seabe
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CPC Code
F01D 25/162
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F01D 9/041
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F01D 9/065
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F01D 17/162
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F04D 29/563
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F04D 29/544
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F02C 9/20
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F01D 9/02
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F01D 17/16
0
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